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Subsonic static longitudinal stability and control characteristics of a wing-body combination having a pointed wing of aspect ratio 2 with constant-percent-chord trailing-edge elevons

机译：翼 - 体组合的亚音速静态纵向稳定性和控制特性，具有纵横比为2的尖翼，具有恒定百分比的弦后缘升力

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Smith, Donald W; Reed, Verlin D;
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年度 1953
页码 1-52
总页数 52
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Transonic static aeroelastic and longitudinal aerodynamic characteristics of a low-aspect-ratio swept wing [J] . Junli Wang AIP Advances . 2019,第4期

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2. Transonic static aeroelastic and longitudinal aerodynamic characteristics of a low-aspect-ratio swept wing [J] . Junli Wang AIP Advances . 2019,第4期

机译：低纵横比后掠翼的跨音速静态气动弹性和纵向气动特性
3. Some compressibility effects on the lee side flow structures of cruciform wing-body configurations with very low aspect ratio wings [J] . S. Tilling, L. Dala, C. Toomer Aerospace science and technology . 2013,第1期

机译：纵横比非常低的十字形机翼构型的下风侧流动结构具有一定的压缩性
4. Longitudinal Flight Stability Augmentation of a Small Blended Wing-Body Aircraft with Canard as Control Surface [C] . Rizal E. M. Nasir, Wahyu Kuntjoro International Conference on Advances in Mechanical Engineering . 2013

机译：纵向飞行稳定性，使用豆类作为控制面的小混纺机翼机架增强
5. THEORETICAL DETERMINATION OF THE PRESSURE DISTRIBUTION ON A LIFTING, SUBSONIC DELTA WING OF ARBITRARY ASPECT RATIO. [D] . SWAIN, CARL EUGENE. 1971

机译：从理论上确定任意纵横比的提升亚音速三角翼上的压力分布。
6. Aerodynamic Characteristics of a Feathered Dinosaur Measured Using Physical Models. Effects of Form on Static Stability and Control Effectiveness [O] . Dennis Evangelista, Griselda Cardona, Eric Guenther-Gleason, -1

机译：使用物理模型测量的羽毛恐龙的空气动力学特性。形式对静态稳定性和控制有效性的影响
7. Flight-Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Reentry Vehicle Configurations With Truncated Bases [O] . Wang K. Charles, Saltzman Edwin J., Iliff Kenneth W. 1999

机译：具有断面基座的七种起降机构和机翼再入飞行器配置的飞行确定的亚音速升力和阻力特性

Subsonic static longitudinal stability and control characteristics of a wing-body combination having a pointed wing of aspect ratio 2 with constant-percent-chord trailing-edge elevons

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